(n)  
Install the trailing edge access panel if you removed the panel.

 (o)  
Move the flap control lever to the UP position to retract the flaps if it is necessary.

 (p)  
Measure the clearance between the spoilers and the flaps.

 (q)  
If the clearance is not in the tolerance, adjust the clearance again.

 S 725-012
 (3)  
Do the test of the No. 0, 1, 8 and 9 ground spoilers.

 S 865-013

 (4)  
Move the FLT CONTROL SPOILER system A and B switches to the ON position.

 S 865-014

 (5)
Remove the systems A and B hydraulic power (Ref 27-62-00/201).

 S 865-015

 (6)  
Remove the electrical power (Ref 24-22-00/201).

 TASK 27-62-91-725-002
 3.  No. 0, 1, 8 and 9 Ground Spoiler Test_____________________________________
 A. Special Tools and Equipment
 (1)  
4MIT65B80307-1 Control Surface Protractor (4 necessary)

 (2)  
F71292-17 Control Surface Protractor Stand Assembly (4 necessary)

 B.
References

 (1)  
24-22-00/201, Manual Control

 (2)  
27-62-00/201, Speed Brake Control System

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737-300/400/500MAINTENANCE MANUAL
 C. Access
 (1)  
Location Zone 101, 102 Control Cabin 307, 407 Wing Trailing Edge Outboard Flap and Spoilers

 D.
Procedure

 S 865-016
 (1)  
Supply the electrical power (Ref 24-22-00/201).

 S 865-017

 (2)  
Supply the system A hydraulic power (Ref 27-62-00/201).

 S 865-018

 (3)  
Move the FLT CONTROL SPOILER system A and B switches to the OFF position.

 S 725-019

 (4)  
Do the test of the ground spoilers No. 0, 1, 8 and 9:

 (a)  
Install the control surface protractor and the stand on the four ground spoilers.

 (b)  
Set the protractors to zero.

 (c)  
Move the speed brake lever in the UP position to lift the spoilers.

 (d)  
Make sure the ground spoilers are up 60 |2 degrees up from the fully retracted position.

 (e)  
Make sure the ground spoilers No. 0 and 9 align in the limit of 2 degrees.

 (f)  
Make sure the ground spoilers No. 1 and 8 align in the limit of 2 degrees.

 (g)  
Move the speed brake lever to the DOWN position to lower the spoilers.

 (h)  
Make sure the ground spoilers are in the fully retracted position.

 (i)  
Remove the control surface protractors and the stands from the spoilers.

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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737-300/400/500MAINTENANCE MANUAL
 E. Put the Airplane Back to Its Usual Condition
 S 865-020
 (1)  
Remove the system A hydraulic power (Ref 27-62-00/201).

 S 865-021

 (2)  
Move the FLT CONTROL SPOILER system A and B switches to the ON position.

 S 865-022

 (3)  
Remove the electrical power (Ref 24-22-00/201).

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 NO. 0, 1, 8 AND 9 GROUND SPOILER ACTUATOR - REMOVAL/INSTALLATION
________________________________________________________________
 1.  General
　
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